CA2913166C - Remplissage d'espace au moyen de matiere intermetallique et de matiere metallique composite - Google Patents

Remplissage d'espace au moyen de matiere intermetallique et de matiere metallique composite Download PDF

Info

Publication number
CA2913166C
CA2913166C CA2913166A CA2913166A CA2913166C CA 2913166 C CA2913166 C CA 2913166C CA 2913166 A CA2913166 A CA 2913166A CA 2913166 A CA2913166 A CA 2913166A CA 2913166 C CA2913166 C CA 2913166C
Authority
CA
Canada
Prior art keywords
fastener
fibers
structural element
structural
alloy
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CA2913166A
Other languages
English (en)
Other versions
CA2913166A1 (fr
Inventor
Adam Franklin Gross
Darrin M. Hansen
Shahriar Khosravani
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Publication of CA2913166A1 publication Critical patent/CA2913166A1/fr
Application granted granted Critical
Publication of CA2913166C publication Critical patent/CA2913166C/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/02—Lightning protectors; Static dischargers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
    • B29C65/562—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using extra joining elements, i.e. which are not integral with the parts to be joined
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112—Single lapped joints
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/01—General aspects dealing with the joint area or with the area to be joined
    • B29C66/05—Particular design of joint configurations
    • B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/13—Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
    • B29C66/131—Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • B29C66/7212—Fibre-reinforced materials characterised by the composition of the fibres
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
    • B29C66/721—Fibre-reinforced materials
    • B29C66/7214—Fibre-reinforced materials characterised by the length of the fibres
    • B29C66/72141—Fibres of continuous length
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/731—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the intensive physical properties of the material of the parts to be joined
    • B29C66/7314—Electrical and dielectric properties
    • B29C66/73141—Electrical conductivity
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/74—Joining plastics material to non-plastics material
    • B29C66/742—Joining plastics material to non-plastics material to metals or their alloys
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
    • B29C70/882—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B1/00—Devices for securing together, or preventing relative movement between, constructional elements or machine parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
    • B22F7/062—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts
    • B22F7/064—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools involving the connection or repairing of preformed parts using an intermediate powder layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/47—Joining single elements to sheets, plates or other substantially flat surfaces
    • B29C66/474—Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially non-flat
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/54—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/731—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the intensive physical properties of the material of the parts to be joined
    • B29C66/7316—Surface properties
    • B29C66/73161—Roughness or rugosity
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7392—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00—General aspects of processes or apparatus for joining preformed parts
    • B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
    • B29C66/7394—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoset
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3002—Superstructures characterized by combining metal and plastics, i.e. hybrid parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
    • F16B2200/93—Fastener comprising feature for establishing a good electrical connection, e.g. electrostatic discharge or insulation feature
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Laminated Bodies (AREA)
  • Connection Of Plates (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

Il est décrit un ensemble structurel dun aéronef qui comprend un élément structurel constitué dun matériau composite qui comprend un matériau matriciel et une pluralité de fibres positionnées pour sétendre à travers le matériau matriciel, dans lequel au moins une partie de la pluralité de fibres est accessible à partir dune surface de lélément structurel. Un élément de fixation fixe lélément structurel à un composant structurel. Une structure métallique comprenant du gallium est positionnée en contact avec une surface de lélément de fixation. La structure métallique sétend de la surface de lélément de fixation et communique avec au moins une partie de ladite au moins une partie de la pluralité de fibres. Il est également décrit un procédé dassemblage dune structure.
CA2913166A 2015-02-05 2015-11-24 Remplissage d'espace au moyen de matiere intermetallique et de matiere metallique composite Active CA2913166C (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/614,656 US20160229552A1 (en) 2015-02-05 2015-02-05 Intermetallic and composite metallic gap filler
US14/614656 2015-02-05

Publications (2)

Publication Number Publication Date
CA2913166A1 CA2913166A1 (fr) 2016-08-05
CA2913166C true CA2913166C (fr) 2020-10-27

Family

ID=55637132

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2913166A Active CA2913166C (fr) 2015-02-05 2015-11-24 Remplissage d'espace au moyen de matiere intermetallique et de matiere metallique composite

Country Status (6)

Country Link
US (1) US20160229552A1 (fr)
EP (1) EP3053679B1 (fr)
JP (1) JP6719218B2 (fr)
CN (2) CN116331503A (fr)
BR (1) BR102015031874B1 (fr)
CA (1) CA2913166C (fr)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5972967B2 (ja) 2012-03-26 2016-08-17 三菱重工業株式会社 燃料タンク、主翼、航空機胴体、航空機及び移動体
RU2605716C2 (ru) * 2012-10-09 2016-12-27 Мицубиси Хеви Индастрис, Лтд. Конструкционный материал для изготовления элементов конструкции, топливного бака, основного крыла и летательного аппарата
JP6071686B2 (ja) 2013-03-26 2017-02-01 三菱重工業株式会社 燃料タンク、主翼、航空機胴体、航空機及び移動体
US10640232B2 (en) * 2016-12-20 2020-05-05 The Boeing Company Conductive fastening system for composite structures
US10518483B2 (en) * 2017-01-25 2019-12-31 The Boeing Company Compound shimming
DE102017203984A1 (de) * 2017-03-10 2018-09-13 Bayerische Motoren Werke Aktiengesellschaft Bolzen für die Befestigung von Komponenten oder den Masseanschluss elektrischer oder elektronischer Komponenten an eine Fahrzeugkarosserie, Bolzenanordnung mit Bolzen und Verfahren zur Ausbildung der Bolzenanordnung
FR3064206B1 (fr) * 2017-03-23 2019-05-03 Centre Technique Des Industries Mecaniques Procede et ensemble de thermoformage
US20180339788A1 (en) * 2017-05-26 2018-11-29 Joe A. Garcia Protective cap and nut gauge for an aircraft fuel tank fastener system
US20190032218A1 (en) * 2017-07-28 2019-01-31 The Boeing Company Process for Adhering Solid Lubricant to Surface of Interference Fit Fastener
US10603844B2 (en) 2017-10-18 2020-03-31 The Boeing Company Apparatus and methods for injecting filler material into a hole in a composite layer
JP6778221B2 (ja) * 2018-01-15 2020-10-28 株式会社Ｓｕｂａｒｕ 締結構造
JP6770987B2 (ja) * 2018-03-12 2020-10-21 株式会社Ｓｕｂａｒｕ 複合材構造体、航空機及び雷電流の誘導方法
US10739389B2 (en) 2018-03-16 2020-08-11 The Boeing Company Systems and methods for measuring the electrical contact resistance at an interface
US10982705B2 (en) * 2018-03-16 2021-04-20 The Boeing Company Method, apparatus and applicator for applying a coating on a surface of a lamination
JP6985192B2 (ja) 2018-03-19 2021-12-22 三菱重工業株式会社 複合材組立体
US11137014B2 (en) 2019-01-08 2021-10-05 The Boeing Company Conductive fastening system and method for improved EME performance
US11181137B2 (en) * 2019-05-20 2021-11-23 The Boeing Company Fastener systems and assemblies for coupling a part to a composite structure, and related methods
US11303047B2 (en) * 2020-01-07 2022-04-12 The Boeing Company Conductively coated fastening systems for full size determinant assembly (FSDA)
US11879488B2 (en) 2020-01-13 2024-01-23 The Boeing Company Lightning damage resistant one sided installation
US11685508B2 (en) * 2020-04-08 2023-06-27 The Boeing Company Systems and methods for constructing a bonded structure
JP2023073774A (ja) * 2021-11-16 2023-05-26 三菱重工業株式会社 複合材料構造体及び複合材料構造体の製造方法
US12070805B2 (en) 2021-12-21 2024-08-27 The Boeing Company Drill spindle accessory for applying a material to an interior sidewall of a hole
JP2025002103A (ja) * 2023-06-21 2025-01-09 三菱重工業株式会社 ロケットの耐雷構造及びこれを備えたロケット並びにロケットの耐雷構造の製造方法
EP4650156A1 (fr) * 2024-05-17 2025-11-19 Airbus S.A.S. Matériau composite renforcé par des fibres, procédé de fabrication d'un matériau composite renforcé par des fibres, composant constitué ou comprenant un matériau composite renforcé par des fibres et une structure de réservoir

Family Cites Families (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3755713A (en) * 1972-07-25 1973-08-28 Boeing Co Electrically conductive surface for aircraft
US4502092A (en) * 1982-09-30 1985-02-26 The Boeing Company Integral lightning protection system for composite aircraft skins
DE3278383D1 (en) * 1982-09-30 1988-05-26 Boeing Co Integral lightning protection system for composite aircraft skins
US4542056A (en) * 1983-08-26 1985-09-17 The Boeing Company Composite structure having conductive surfaces
US4755904A (en) * 1986-06-06 1988-07-05 The Boeing Company Lightning protection system for conductive composite material structure
GB8628555D0 (en) * 1986-11-28 1987-01-07 British Aerospace Anti lightning strike fasteners
US4920449A (en) * 1988-01-19 1990-04-24 The Boeing Company Conductive bonding of composite structures
US4905931A (en) * 1988-02-18 1990-03-06 The Boeing Company Arc suppression around fasteners
US5225157A (en) * 1989-07-19 1993-07-06 Microelectronics And Computer Technology Corporation Amalgam composition for room temperature bonding
GB8924231D0 (en) * 1989-10-27 1989-12-13 British Aerospace Carbon fibre composite structures
US5170930A (en) * 1991-11-14 1992-12-15 Microelectronics And Computer Technology Corporation Liquid metal paste for thermal and electrical connections
US5445308A (en) * 1993-03-29 1995-08-29 Nelson; Richard D. Thermally conductive connection with matrix material and randomly dispersed filler containing liquid metal
US5328087A (en) * 1993-03-29 1994-07-12 Microelectronics And Computer Technology Corporation Thermally and electrically conductive adhesive material and method of bonding with same
FR2718706B1 (fr) * 1994-04-15 1996-06-14 Aerospatiale Structure anti-étincelage, notamment pour aéronef.
GB9411006D0 (en) * 1994-06-02 1994-07-20 British Aerospace Method of fastening composite aircraft skins
FR2765066B1 (fr) * 1997-06-20 1999-08-20 Aerospatiale Structure anti-etincelage, notamment pour aeronef
US6027575A (en) * 1997-10-27 2000-02-22 Ford Motor Company Metallic adhesive for forming electronic interconnects at low temperatures
US6327132B1 (en) * 1998-06-10 2001-12-04 Aerospatiale Matra Spark resistant structure, in particular for aircraft
CN1408494A (zh) * 2002-08-28 2003-04-09 丁刚 挤压铸渗烧结工艺生产复合材料及设备
DE602004002482T2 (de) * 2003-05-30 2007-02-01 Bae Systems Plc Verbundstruktur-blitzschlagschutz
US7554785B2 (en) * 2004-03-23 2009-06-30 The Boeing Company Lightning damage protection for composite aircraft
US7686905B2 (en) * 2005-09-06 2010-03-30 The Boeing Company Copper grid repair technique for lightning strike protection
US7551656B2 (en) * 2006-03-29 2009-06-23 Lockheed Martin Coherent Technologies, Inc. Low stress optics mount using thermally conductive liquid metal or gel
US7898785B2 (en) * 2006-12-07 2011-03-01 The Boeing Company Lightning protection system for an aircraft composite structure
DE102007003276B4 (de) * 2007-01-23 2013-11-28 Airbus Operations Gmbh Luft- und Raumfahrzeug mit einem CFK-Bauteil und einem Metallbauteil, wobei das CFK-Bauteil und das Metallbauteil über wenigstens ein Verbindungselement mit einem Verbindungsabschnitt miteinander verbunden sind
JP2008197296A (ja) * 2007-02-13 2008-08-28 Sony Corp エレクトロウェッティングデバイス及びその製造方法
JP2008285115A (ja) * 2007-05-21 2008-11-27 Mitsubishi Heavy Ind Ltd 航空機組立品およびその製造方法
US7966711B2 (en) * 2007-08-14 2011-06-28 The Boeing Company Method and apparatus for fastening components using a composite two-piece fastening system
JP4719203B2 (ja) * 2007-09-28 2011-07-06 三菱重工業株式会社 耐雷ファスナ
EP2210001B1 (fr) * 2007-10-16 2017-08-02 Fatigue Technology, Inc. Ensemble attache expansible à collier déformé
US7721996B2 (en) * 2007-11-13 2010-05-25 The Boeing Company Fabrication and installation of preformed dielectric inserts for lightning strike protection
FR2924686B1 (fr) * 2007-12-11 2010-05-14 Airbus France Systeme parafoudre et aeronef comportant un tel systeme.
JP5055178B2 (ja) * 2008-03-24 2012-10-24 三菱重工業株式会社 航空機組立品
US8834766B2 (en) * 2008-07-31 2014-09-16 Airbus Operations S.L. Protection of elements in composite material
US8382413B2 (en) * 2008-11-17 2013-02-26 The Boeing Company Conductive sleeved fastener assembly
EP2325848B1 (fr) * 2009-11-11 2017-07-19 Samsung Electronics Co., Ltd. Colle conductrice et cellule solaire
US20120019973A1 (en) * 2010-06-14 2012-01-26 Aurora Flight Sciences Corporation Method and apparatus for grounding a composite aircraft structure
US8668847B2 (en) * 2010-08-13 2014-03-11 Samsung Electronics Co., Ltd. Conductive paste and electronic device and solar cell including an electrode formed using the conductive paste
US8791375B2 (en) * 2010-12-16 2014-07-29 The Boeing Company Electrically conductive bushing connection to structure for current path
US8783735B2 (en) * 2011-10-24 2014-07-22 The Boeing Company Conductance on hydraulic fittings using a soft metal interlayer
JP5713980B2 (ja) * 2012-10-15 2015-05-07 三菱航空機株式会社 耐雷ファスナおよび航空機
EP2730508B1 (fr) * 2012-11-12 2016-09-14 Airbus Operations GmbH Panneau de carénage/garniture et procédé de mesure de la résistance de liaison électrique d'un panneau de carénage/garniture
US9343824B2 (en) * 2013-02-04 2016-05-17 The Boeing Company Sleeved fastener assembly
US9331402B2 (en) * 2013-02-04 2016-05-03 The Boeing Company Conductive sleeved fastener assembly
US9682533B1 (en) * 2014-09-09 2017-06-20 Hrl Laboratories, Llc Methods to form electrical-mechanical connections between two surfaces, and systems and compositions suitable for such methods

Also Published As

Publication number Publication date
EP3053679B1 (fr) 2019-12-18
CN105857629A (zh) 2016-08-17
BR102015031874B1 (pt) 2020-10-27
CN116331503A (zh) 2023-06-27
JP2016175634A (ja) 2016-10-06
US20160229552A1 (en) 2016-08-11
JP6719218B2 (ja) 2020-07-08
EP3053679A1 (fr) 2016-08-10
BR102015031874A2 (pt) 2017-01-24
CA2913166A1 (fr) 2016-08-05

Similar Documents

Publication Publication Date Title
CA2913166C (fr) Remplissage d'espace au moyen de matiere intermetallique et de matiere metallique composite
US8322958B2 (en) Fasteners with conforming sleeves
DE4341598B4 (de) Kompositteilchen, diese enthaltende Zusammensetzungen, Verfahren zum Herstellen derselben und Verwendungen
DE60221079T3 (de) Zinn-Silberbeschichtungen
DE102012216461A1 (de) Korrosionsschutz für Magnesiumkomponenten durch eine Befestigungsmittelisolierung
BR112014021234B1 (pt) Método, prendedor, e, sistema de preensão
EP1730813A1 (fr) Procede pour relier un element de raccordement a un conducteur electrique en aluminium et conducteur electrique fabrique selon ce procede
RU2605716C2 (ru) Конструкционный материал для изготовления элементов конструкции, топливного бака, основного крыла и летательного аппарата
DE3446780A1 (de) Verfahren und verbindungswerkstoff zum metallischen verbinden von bauteilen
US4478915A (en) Corrosion resistant shim for electrically joining incompatible materials
DE1494994A1 (de) Metallgefuellter,elektrisch leitender Kunststoff
EP2058081A2 (fr) Pâte de métal liquide
DE102014117410B4 (de) Elektrisches Kontaktelement, Einpressstift, Buchse und Leadframe
DE112008003131T5 (de) Korrosionsschutzmethode und Apparatur zur Stahlverstärkung in Betonkonstruktionen
DE102012001859B4 (de) Verbindungsanordnung und Verfahren zum Verbinden wenigstens eines ersten Bauteils aus einem kohlefaserverstärkten Verbundwerkstoff mit wenigstens einem zweiten Bauteil
DE102015225077B4 (de) Leitfähiger Klebstoff und Klebeverfahren für ein Verbundmaterial unter Verwendung des leitfähigen Klebstoffs
EP2979976B1 (fr) Réservoir de carburant, ailes principales, fuselage d'aéronef, aéronef et corps mobile
Hua et al. Electrochemical corrosion and electrochemical migration of 64Sn-35Bi-1Ag solder doping with xGe on printed circuit boards
Sancaktar et al. Conduction efficiency and strength of electronically conductive adhesive joints
DE102011075926A1 (de) Hybridbauteil und Verfahren zur Herstellung eines Hybridbauteils
EP3260377B1 (fr) Dispositif de production de corps structurel et procédé de production de corps structurel
DE102010055949A1 (de) Verbindungsanordnung
JP2021181223A (ja) 伝導性複合材及び伝導性複合材を製造するための方法
DE10200564B4 (de) Blitzschutzeinrichtung an faserverstärkten Bauteilen für mittels lösbaren Bolzenverbindungen entfernbare Verschluss-Deckel
Yim et al. Effect of multi-walled carbon nanotube (MWCNT) concentration on thermomechanical reliability of MWCNT-reinforced solderable isotropic polymer nanocomposites

Legal Events

Date Code Title Description
EEER Examination request

Effective date: 20171127